An electromechanical and/or electronic, self-contained, automatically controlling device. It is designed to be mounted on the body or contained within the guidance section of an air launched missile. Its funtion is to measure linear acceleration, angular rate, delta-velocity and delta-altitude. It contains sensors, accelerometers, gyroscopes and the like. Excludes inertial navication system.
Classification: Parts for guided missiles
NSN 5905-00-391-6398
NSN 5998-00-161-0099
NSN 6135-01-322-4655
NSN 5910-01-041-1298
NSN 7035-00-155-9513
NSN 5895-00-876-9626
NSN 6220-00-546-1836
NSN 6150-00-288-6245
NSN 5990-01-364-8405
NSN 5960-01-363-3805
NSN 5945-01-634-0588
NSN 5998-01-640-8655